FR2891245B1 - METHOD FOR MOUNTING AN AIRCRAFT ENGINE ON A RIGID STRUCTURE OF A MOTOR ATTACHMENT MAT - Google Patents
METHOD FOR MOUNTING AN AIRCRAFT ENGINE ON A RIGID STRUCTURE OF A MOTOR ATTACHMENT MATInfo
- Publication number
- FR2891245B1 FR2891245B1 FR0552868A FR0552868A FR2891245B1 FR 2891245 B1 FR2891245 B1 FR 2891245B1 FR 0552868 A FR0552868 A FR 0552868A FR 0552868 A FR0552868 A FR 0552868A FR 2891245 B1 FR2891245 B1 FR 2891245B1
- Authority
- FR
- France
- Prior art keywords
- engine
- rigid structure
- aircraft engine
- mounting
- orifice
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
- B64D27/404—Suspension arrangements specially adapted for supporting vertical loads
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
- B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Vibration Prevention Devices (AREA)
- Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
- Connection Of Plates (AREA)
- Automobile Manufacture Line, Endless Track Vehicle, Trailer (AREA)
- Hybrid Electric Vehicles (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
- Motor Or Generator Frames (AREA)
Abstract
A method to mount an aircraft engine on a rigid structure of an engine mount, includes securing, on the structure, an attachment body for an engine attachment, the attachment body configured to lie against a contact surface of the rigid structure oriented forwardly, and secured to the structure by at least one shear pin passing through a first and a second primary orifice. The securing of the body includes: pre-positioning the engine relative to the engine mount to place the first orifice opposite the second orifice, and inserting a pin fitted with a convex centering head through the two orifices, so that the pin forms the shear pin.
Priority Applications (11)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0552868A FR2891245B1 (en) | 2005-09-26 | 2005-09-26 | METHOD FOR MOUNTING AN AIRCRAFT ENGINE ON A RIGID STRUCTURE OF A MOTOR ATTACHMENT MAT |
JP2008531713A JP5047973B2 (en) | 2005-09-26 | 2006-09-22 | Method for assembling an aircraft engine to a rigid structure of an engine mount |
CNB2006800338238A CN100519341C (en) | 2005-09-26 | 2006-09-22 | Method for mounting an aircraft engine on a rigid structure of a strut for locking the engine |
US12/067,190 US8083176B2 (en) | 2005-09-26 | 2006-09-22 | Method for mounting an aircraft engine on a rigid structure of a strut for locking the engine |
BRPI0616138-3A BRPI0616138A2 (en) | 2005-09-26 | 2006-09-22 | Mounting process of an aircraft engine on a rigid structure of an engine mounting bracket |
PCT/EP2006/066633 WO2007033993A1 (en) | 2005-09-26 | 2006-09-22 | Method for mounting an aircraft engine on a rigid structure of a strut for locking the engine |
RU2008116565/11A RU2401221C2 (en) | 2005-09-26 | 2006-09-22 | Method of mounting aicraft engine on its suspension rigid pylon |
DE602006011034T DE602006011034D1 (en) | 2005-09-26 | 2006-09-22 | METHOD FOR ASSEMBLING A MOTOR VEHICLE ON A RIGID STRUCTURE FOR SECURING THE ENGINE |
CA2623758A CA2623758C (en) | 2005-09-26 | 2006-09-22 | Method to mount an aircraft engine on a rigid structure of an engine mount |
EP06793751A EP1928739B1 (en) | 2005-09-26 | 2006-09-22 | Method for mounting an aircraft engine on a rigid structure of a strut for locking the engine |
AT06793751T ATE451302T1 (en) | 2005-09-26 | 2006-09-22 | METHOD OF MOUNTING AN AIRCRAFT ENGINE ON A RIGID STRUT STRUCTURE FOR SECURING THE ENGINE |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0552868A FR2891245B1 (en) | 2005-09-26 | 2005-09-26 | METHOD FOR MOUNTING AN AIRCRAFT ENGINE ON A RIGID STRUCTURE OF A MOTOR ATTACHMENT MAT |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2891245A1 FR2891245A1 (en) | 2007-03-30 |
FR2891245B1 true FR2891245B1 (en) | 2007-10-26 |
Family
ID=36581620
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0552868A Expired - Fee Related FR2891245B1 (en) | 2005-09-26 | 2005-09-26 | METHOD FOR MOUNTING AN AIRCRAFT ENGINE ON A RIGID STRUCTURE OF A MOTOR ATTACHMENT MAT |
Country Status (11)
Country | Link |
---|---|
US (1) | US8083176B2 (en) |
EP (1) | EP1928739B1 (en) |
JP (1) | JP5047973B2 (en) |
CN (1) | CN100519341C (en) |
AT (1) | ATE451302T1 (en) |
BR (1) | BRPI0616138A2 (en) |
CA (1) | CA2623758C (en) |
DE (1) | DE602006011034D1 (en) |
FR (1) | FR2891245B1 (en) |
RU (1) | RU2401221C2 (en) |
WO (1) | WO2007033993A1 (en) |
Families Citing this family (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2891248B1 (en) * | 2005-09-28 | 2009-05-01 | Airbus France Sas | ENGINE ASSEMBLY FOR AN AIRCRAFT COMPRISING AN ENGINE AND A MACHINE FOR ATTACHING SUCH A MOTOR |
FR2928180B1 (en) | 2008-02-28 | 2010-04-02 | Airbus France | AIRCRAFT ENGINE ASSEMBLY COMPRISING AN ANNULAR EFFORTS TRANSFER STRUCTURE SURROUNDING THE CENTRAL HOUSING OF A TURBOJET ENGINE. |
FR2928136B1 (en) * | 2008-02-28 | 2010-04-02 | Airbus France | AIRCRAFT ENGINE ASSEMBLY COMPRISING ENGINE FASTENERS DEPORTED DOWN TO THE BLOWER HOUSING. |
FR2928181B1 (en) * | 2008-02-28 | 2010-04-02 | Airbus France | AIRCRAFT ENGINE ASSEMBLY COMPRISING A TURBOJET ENGINE WITH REINFORCING STRUCTURES CONNECTING THE BLOWER HOUSING TO THE CENTRAL CASING. |
FR2928347B1 (en) * | 2008-03-07 | 2010-06-25 | Aircelle Sa | HANGING STRUCTURE FOR TURBOJET ENGINE |
FR2965548B1 (en) * | 2010-10-01 | 2012-10-19 | Airbus Operations Sas | AIRCRAFT ENGINE ATTACHMENT MAT COMPRISING TWO FRONT SAILING ATTACHES WITH ORTHOGONAL SHEARING PONDS |
FR3000467A1 (en) * | 2012-12-28 | 2014-07-04 | Airbus Operations Sas | THREE POINTS MANILA WITH VIBRATION FILTRATION CAPACITY AND AIRCRAFT ENGINE ATTACHMENT EQUIPPED WITH SUCH A MANILA |
CA2918320C (en) | 2013-07-26 | 2018-05-15 | Mra Systems, Inc. | Aircraft engine pylon |
FR3015434B1 (en) * | 2013-12-23 | 2017-12-08 | Snecma | TURBOMACHINE SUSPENSION |
JP6533043B2 (en) * | 2014-08-25 | 2019-06-19 | 三菱航空機株式会社 | Aircraft engine installation method |
FR3027873B1 (en) * | 2014-11-03 | 2016-12-23 | Airbus Operations Sas | FRONT ENGINE ATTACHMENT FOR AN AIRCRAFT ENGINE |
CN110182373B (en) * | 2015-01-07 | 2023-01-10 | 洛德公司 | Bearing assembly for aircraft engine mount |
FR3040076B1 (en) * | 2015-08-13 | 2017-08-11 | Airbus Operations Sas | AIRCRAFT ENGINE ASSEMBLY COMPRISING A PRIMARY STRUCTURE OF A COUPLING MAT EQUIPPED WITH A BOX EXTENSION COMPRISING TWO PARTS IN GLOBAL ARCEAU SHAPE |
FR3061480B1 (en) * | 2016-12-30 | 2019-05-31 | Airbus Operations | AIRCRAFT ENGINE ASSEMBLY COMPRISING A FRONT ENGINE ATTACHMENT FACILITATING ITS ASSEMBLY |
FR3065442B1 (en) * | 2017-04-25 | 2021-03-19 | Airbus Operations Sas | ENGINE ASSEMBLY FOR AIRCRAFT INCLUDING A FRONT ENGINE ATTACHMENT INTEGRATED IN THE HOUSING OF THE MAST |
FR3084339A1 (en) * | 2018-07-30 | 2020-01-31 | Airbus Operations | ASSEMBLY FOR AN AIRCRAFT, THE ASSEMBLY COMPRISING A MAT AND A FRONT ENGINE MOUNT |
FR3085874A1 (en) * | 2018-09-14 | 2020-03-20 | Airbus Operations | BORE CENTERING TOOL AND METHOD FOR CENTERING THE BORES OF AN AIRCRAFT ENGINE MOUNT USING THE SAME |
FR3091519A1 (en) | 2019-01-09 | 2020-07-10 | Airbus Operations (S.A.S.) | Aircraft engine mount comprising at least one fork-type translational immobilization system of a shear pin, method of mounting said engine mount and aircraft comprising said engine mount |
FR3091520A1 (en) | 2019-01-09 | 2020-07-10 | Airbus Operations (S.A.S.) | Aircraft engine fastener comprising at least one system for immobilizing in translation a shear pin comprising a cover plate, method for mounting said engine fastener and aircraft comprising said engine fastener |
FR3093142A1 (en) * | 2019-02-22 | 2020-08-28 | Airbus Operations | Set of parts assembled by a through shaft that can be mounted in case of approximate alignment between the parts |
FR3093995A1 (en) * | 2019-03-18 | 2020-09-25 | Airbus Operations (S.A.S.) | Rear engine attachment of an aircraft having a reduced overall width and aircraft comprising at least one such rear engine attachment |
FR3106126B1 (en) * | 2020-01-10 | 2022-01-07 | Safran Aircraft Engines | ASSEMBLY BETWEEN AN AIRCRAFT PYLON AND A TURBOMACHINE |
CN111746805B (en) * | 2020-05-21 | 2022-02-18 | 卓尔飞机制造(武汉)有限公司 | Novel aircraft engine installing support |
US11428160B2 (en) | 2020-12-31 | 2022-08-30 | General Electric Company | Gas turbine engine with interdigitated turbine and gear assembly |
FR3124491A1 (en) * | 2021-06-29 | 2022-12-30 | Airbus Operations (S.A.S.) | Aircraft thruster assembly comprising a front engine attachment comprising a transverse beam partially positioned facing a front transverse reinforcement of a primary structure of a mast |
FR3126695A1 (en) * | 2021-09-03 | 2023-03-10 | Airbus Operations | FRONT ENGINE MOUNT SYSTEM FOR AN AIRCRAFT ENGINE THAT FEATURES A COMPACT STRUCTURE |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2635751B1 (en) * | 1988-09-01 | 1991-01-04 | Snecma | DEVICE FOR FIXING A SUSPENSION LINK OF A TURBO-JET |
GB9125011D0 (en) * | 1991-11-25 | 1992-01-22 | Rolls Royce Plc | A mounting arrangement for a gas turbine engine |
US5351930A (en) * | 1992-08-11 | 1994-10-04 | Lord Corporation | Mounting for engines and the like |
US5649417A (en) * | 1995-03-24 | 1997-07-22 | The Boeing Company | Fail-safe engine mount system |
FR2755944B1 (en) * | 1996-11-21 | 1998-12-24 | Snecma | REDUNDANT FRONT SUSPENSION FOR TURBOMACHINE |
FR2755943B1 (en) * | 1996-11-21 | 1998-12-24 | Snecma | REDUNDANT FRONT SUSPENSION FOR TURBOMACHINE |
US6330995B1 (en) * | 2000-02-29 | 2001-12-18 | General Electric Company | Aircraft engine mount |
FR2818614B1 (en) * | 2000-12-21 | 2003-01-31 | Snecma Moteurs | SUSPENSION PART OF A TURBO-JET |
FR2828167B1 (en) * | 2001-07-31 | 2003-11-21 | Airbus France | DEVICE FOR HANGING AN ENGINE ON AN AIRCRAFT |
US6517027B1 (en) * | 2001-12-03 | 2003-02-11 | Pratt & Whitney Canada Corp. | Flexible/fixed support for engine cowl |
FR2836672B1 (en) * | 2002-03-04 | 2004-06-04 | Airbus France | MATCH FOR HANGING AN ENGINE UNDER AN AIRCRAFT |
FR2855494B1 (en) * | 2003-05-27 | 2006-09-22 | Snecma Moteurs | AIRCRAFT ENGINE REAR HITCHING DEVICE |
FR2883839B1 (en) * | 2005-03-29 | 2007-06-29 | Snecma Moteurs Sa | REAR SUSPENSION OF TURBOREACTOR |
US7654093B2 (en) * | 2005-09-26 | 2010-02-02 | Pratt & Whitney Canada Corp. | Method of adjusting a triggering clearance and a trigger |
FR2905932B1 (en) * | 2006-09-20 | 2008-12-05 | Airbus France Sa | ARRANGEMENT FOR ATTACHING DEVICE FOR ATTACHING AN AIRCRAFT ENGINE |
-
2005
- 2005-09-26 FR FR0552868A patent/FR2891245B1/en not_active Expired - Fee Related
-
2006
- 2006-09-22 CN CNB2006800338238A patent/CN100519341C/en not_active Expired - Fee Related
- 2006-09-22 CA CA2623758A patent/CA2623758C/en not_active Expired - Fee Related
- 2006-09-22 AT AT06793751T patent/ATE451302T1/en not_active IP Right Cessation
- 2006-09-22 WO PCT/EP2006/066633 patent/WO2007033993A1/en active Application Filing
- 2006-09-22 US US12/067,190 patent/US8083176B2/en not_active Expired - Fee Related
- 2006-09-22 BR BRPI0616138-3A patent/BRPI0616138A2/en active Search and Examination
- 2006-09-22 JP JP2008531713A patent/JP5047973B2/en not_active Expired - Fee Related
- 2006-09-22 DE DE602006011034T patent/DE602006011034D1/en active Active
- 2006-09-22 EP EP06793751A patent/EP1928739B1/en not_active Ceased
- 2006-09-22 RU RU2008116565/11A patent/RU2401221C2/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
FR2891245A1 (en) | 2007-03-30 |
CN100519341C (en) | 2009-07-29 |
CA2623758C (en) | 2013-12-17 |
RU2401221C2 (en) | 2010-10-10 |
US20080223983A1 (en) | 2008-09-18 |
ATE451302T1 (en) | 2009-12-15 |
EP1928739B1 (en) | 2009-12-09 |
JP2009509826A (en) | 2009-03-12 |
EP1928739A1 (en) | 2008-06-11 |
DE602006011034D1 (en) | 2010-01-21 |
CN101263055A (en) | 2008-09-10 |
RU2008116565A (en) | 2009-11-10 |
BRPI0616138A2 (en) | 2011-06-07 |
WO2007033993A1 (en) | 2007-03-29 |
CA2623758A1 (en) | 2007-03-29 |
JP5047973B2 (en) | 2012-10-10 |
US8083176B2 (en) | 2011-12-27 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR2891245B1 (en) | METHOD FOR MOUNTING AN AIRCRAFT ENGINE ON A RIGID STRUCTURE OF A MOTOR ATTACHMENT MAT | |
FR2915176B1 (en) | ENGINE ATTACHING MACHINE FOR AN AIRCRAFT HAVING A REAR ENGINE ATTACHMENT HAVING A BARREL NUT | |
FR2887851B1 (en) | ENGINE ATTACHING MAT FOR AN AIRCRAFT | |
FR2891243B1 (en) | ENGINE ATTACHING MAT FOR AN AIRCRAFT | |
FR2903382B1 (en) | DEVICE FOR HITCHING AN AIRCRAFT ENGINE COMPRISING TWO PIVOT RETRACTORS WITH EMBOITEMENT TRANSVERSE | |
DE602005006147D1 (en) | PASSENGER SIDING UNIT FOR PLANE AND AIRCRAFT THEREOF | |
FR2891242B1 (en) | TURBOREACTOR FOR AIRCRAFT, AIRCRAFT PROVIDED WITH SUCH A TURBOJET ENGINE, AND METHOD FOR FITTING SUCH A TURBO AIRBORNE ON AN AIRCRAFT | |
MY147071A (en) | Motorcycle | |
CN205639199U (en) | Sheet metal working of plastics quick connect structure | |
ATE416975T1 (en) | AIRCRAFT ENGINE UNIT | |
DE602006005387D1 (en) | ENGINE ARRANGEMENT FOR PLANE | |
KR20070102957A (en) | Piping fixing structure | |
WO2007055987A3 (en) | Support element for strengthening connection between a tool and its holder | |
ATE367951T1 (en) | FASTENING DEVICE FOR A MONITOR ON A VEHICLE SEAT | |
JP2004100789A (en) | Vehicle power source mount structure | |
JPS5836723A (en) | Fitting and holding construction for radiator | |
WO2009037942A1 (en) | Compressor | |
CN204437172U (en) | A kind of ECU damper mechanism | |
ATE519928T1 (en) | SHOCK MOUNTING BRACKET AND STRAP SEAT VEHICLE WITH IT | |
BRPI0419174A (en) | a mounting system for a stay (tie rod) in (v) on a large vehicle | |
KR20120069967A (en) | Mounting apparatus of fuel tank for automobile | |
WO2007036520A3 (en) | Engine mounting structure for an aircraft engine | |
FR2903457B1 (en) | DEVICE FOR ENHANCING NOISE AND VIBRATION DUE TO INJECTORS IN A VEHICLE ENGINE | |
CN202088814U (en) | Mounting structure of constant speed drive shaft | |
JP2012180800A (en) | Air intake duct |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |
Effective date: 20110531 |